Machine Design: cram pack

Formula sheets, the key method steps for every topic and 12 practice problems, with full solutions at the back.

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1Formulas and methods

Gears & gear trains

Meshing gears
n1·N1 = n2·N2
Torque
T2 = T1·(N2/N1)·η
Power
P = T·ω, ω = 2π·n/60
Compound train
total ratio = product of the stage ratios

Torsion of shafts

Shear stress
τ = T·r/J
Solid shaft
J = πd⁴/32
Hollow shaft
J = π(D⁴ − d⁴)/32
Angle of twist
φ = TL/(GJ)
Power
P = T·ω = 2πnT/60

Method

  1. Find the polar moment of area: J = πd⁴/32 for a solid shaft.
  2. Shear stress at the surface: τ = T·r/J, with r the outer radius.
  3. Angle of twist: φ = TL/(GJ) in radians.
  4. If power is given, find the torque first with P = T·ω, ω = 2πn/60.

Mohr’s circle & stress transformation

Centre
C = (σx + σy)/2
Radius
R = √(((σx − σy)/2)² + τxy²)
Principal stresses
σ1,2 = C ± R
Principal direction
tan 2θp = 2τxy/(σx − σy)
Inclined plane
σθ = C + (σx − σy)/2·cos 2θ + τxy·sin 2θ

Method

  1. Calculate the centre of Mohr’s circle: C = (σx + σy)/2.
  2. Calculate the radius: R = √(((σx − σy)/2)² + τxy²).
  3. The principal stresses are C ± R and the largest in-plane shear stress is R.
  4. Angles on the circle are double the angles on the element: tan 2θp = 2τxy/(σx − σy).

Axial stress & strain

Normal stress
σ = F/A
Strain
ε = ΔL/L
Hooke’s law
σ = E·ε
Elongation
ΔL = FL/(EA)
Thermal strain
εT = α·ΔT

Column buckling

Euler load
Pcr = π²EI/(KL)²
Effective length factor
K = 1 pinned–pinned, 0.5 fixed–fixed, 0.7 fixed–pinned, 2 fixed–free
Critical stress
σcr = Pcr/A
Slenderness
λ = KL/r, r = √(I/A)

Mechanical vibrations

Natural frequency
ωn = √(k/m), fn = ωn/(2π)
From static deflection
ωn = √(g/δst)
Critical damping
cc = 2√(km) = 2mωn
Damping ratio
ζ = c/cc
Damped frequency
ωd = ωn√(1 − ζ²)
Logarithmic decrement
δ = (1/n)·ln(x0/xn), ζ = δ/√(4π² + δ²)
Springs in parallel
k = k1 + k2
Springs in series
1/k = 1/k1 + 1/k2

2Practice problems

1.Gears & gear trainsMedium
N1​ = 24, m = 4 mm

A 22 kW motor running at 1450 rpm drives a pinion with 24 teeth and a module of 4 mm. Find the tangential force Ft on the pinion teeth.

P = 22 kWn = 1450 rpmN1 = 24m = 4 mm
Ft = N
2.Gears & gear trainsHard
d1​ = 80 mmd2​ = 500 mm960 rpmC = 500 mmT1​ = 2000 NT2​P = ?

An open belt connects an 80 mm driving pulley at 960 rpm to a 500 mm pulley; the centres are 500 mm apart. The coefficient of friction is 0.25 and the tight-side tension may not exceed 2000 N. Find the largest power P the belt can transmit without slipping, in kW (ignore centrifugal effects).

d1 = 80 mmn1 = 960 rpmd2 = 500 mmC = 500 mmμ = 0.25T1 = 2000 N
P = kW
3.Torsion of shaftsMedium
d = 15 mmT = 20 N·m250 mmφ = 1.48°

In a torsion test, a solid specimen of diameter 15 mm is twisted by a torque of 20 N·m. The two ends of a gauge length of 250 mm rotate 1.48° relative to each other (the material is still elastic). Find the shear modulus G of the material.

T = 20 N·md = 15 mmL = 250 mmφ = 1.48°
G = GPa
4.Torsion of shaftsHard
Td = ?

A solid shaft must transmit 30 kW at 750 rpm without the shear stress exceeding 80 MPa. Find the smallest diameter d that works.

P = 30 kWN = 750 rpmτallow = 80 MPa
d = mm
5.Mohr’s circle & stress transformationMedium
σx​ = −10σy​ = 10τxy​ = −20MPa

A point has σₓ = −10 MPa, σᵧ = 10 MPa and τₓᵧ = −20 MPa (tension positive). The element is rotated 30° clockwise. Find the normal stress σy′ on the faces of the rotated element that are perpendicular to the rotated y′-axis.

σx = −10 MPaσy = 10 MPaτxy = −20 MPaθ = -30°
σy′ = MPa
6.Mohr’s circle & stress transformationHard
σx​ = 50σy​ = 90τxy​ = 40MPa

A point in a loaded part has σₓ = 50 MPa, σᵧ = 90 MPa and τₓᵧ = 40 MPa (tension positive). Find the shear stress τθ on a plane whose normal is rotated 20° counter-clockwise from the x-axis (positive in the same sense as τₓᵧ).

σx = 50 MPaσy = 90 MPaτxy = 40 MPaθ = 20°
τθ = MPa
7.Axial stress & strainMedium
P = ?12500 mm200 mmØ20Ø40δ = 0.4 mm

A bar is made of a steel segment (diameter 20 mm, length 500 mm, E = 200 GPa) joined end to end with a segment made of brass (diameter 40 mm, length 200 mm, E = 100 GPa). It is fixed at one end and pulled at the other. Find the axial load P that stretches it by 0.4 mm in total.

segment 1: steel, Ø20 mm, 500 mm, E = 200 GPasegment 2: brass, Ø40 mm, 200 mm, E = 100 GPaδ = 0.4 mm
P = kN
8.Axial stress & strainHard
30 kN12500 mm400 mmØ25Ø60σ2​ = ?

A steel segment (diameter 25 mm, length 500 mm, E = 200 GPa) and a segment made of aluminium (diameter 60 mm, length 400 mm, E = 70 GPa) are joined end to end and fixed between two rigid walls. An axial load of 30 kN acts at the joint, towards segment 2. Find the magnitude of the stress σ2 in segment 2.

segment 1: steel, Ø25 mm, 500 mm, E = 200 GPasegment 2: aluminium, Ø60 mm, 400 mm, E = 70 GPaP = 30 kN
σ2 = MPa
9.Column bucklingMedium
PL = 3 md = 30 mmcross-section

A column of length L made of aluminium is pinned at both ends. Using Euler’s formula, find its critical buckling load Pcr.

L = 3 mE = 70 GPa (aluminium)d = 30 mm
Pcr = kN
10.Column bucklingHard
P = 30 kNL = 4 md = ?cross-section

A solid round column of length L made of steel is fixed at the base and free at the top. It must carry 30 kN with a factor of safety of 2 against buckling. Find the smallest diameter d.

P = 30 kNn = 2L = 4 mE = 200 GPa (steel)
d = mm
11.Mechanical vibrationsMedium
tx40 mm4 cycles3.2 mm

In a free-vibration test of a damped mass–spring system, a displacement peak of 40 mm is followed 4 cycles later by a peak of 3.2 mm. Find the damping ratio ζ.

x0 = 40 mmx4 = 3.2 mmn = 4
ζ =
12.Mechanical vibrationsHard
k1​ = 12k2​ = 5k3​ = 25m = 40 kg

A 40 kg mass hangs from spring k₃ = 25 kN/m. The top of k₃ is attached to a rigid bar that hangs from two springs side by side, k₁ = 12 kN/m and k₂ = 5 kN/m; the bar stays level. Ignore damping and the masses of the springs and bar. Find the natural frequency fn of vertical vibration in Hz.

m = 40 kgk1 = 12 kN/mk2 = 5 kN/mk3 = 25 kN/m
fn = Hz

3Solutions

1.Gears & gear trains

Answer: Ft = 3018 N

Gear geometry: the module m sets the tooth size. A gear with N teeth has a pitch diameter d = m·N, two meshing gears have the same module, and their centre distance is a = (d₁ + d₂)/2 = m·(N₁ + N₂)/2. The pitch-line speed is v = π·d·n/60, and the tangential tooth force follows from the torque: Ft = 2T/d.

Torque on the pinion

ω = 2π·1450/60 = 151.8 rad/s
T = P/ω = 22000/151.8 = 144.9 N·m

Pitch diameter

d = m·N = 4·24 = 96 mm

Tangential force

Ft = 2T/d = 2·144.9/0.096 = 3018 N

Answer

Ft = 3018 N
2.Gears & gear trains

Answer: P = 3.488 kW

Belt drives: without slip, both pulleys have the same rim speed v = π·d·n/60, so n₁·d₁ = n₂·d₂ and the speed ratio is d₂/d₁. Slip s makes the driven pulley a little slower: n₂ = n₁·(d₁/d₂)·(1 − s). The power transmitted is P = (T₁ − T₂)·v, with T₁ the tension on the tight side and T₂ on the slack side. Friction limits the ratio of the tensions: T₁/T₂ = eμθ, where θ is the angle of wrap in radians on the smaller pulley; for an open belt θ = π − 2·asin((d₂ − d₁)/(2C)) with centre distance C.

Angle of wrap

θ = 2.275 rad

Slack-side tension

eμθ = e0.5687 = 1.766, T₂ = 2000/1.766 = 1133 N

Power

P = (2000 − 1133)·4.021 = 3.488 kW

Answer

P = 3.488 kW
3.Torsion of shafts

Answer: G = 38.95 GPa

Torsion of circular shafts: shear stress grows linearly from zero at the centre to τmax = T·r/J at the surface, with J = πd⁴/32 for a solid shaft and J = π(do⁴ − di⁴)/32 for a hollow one. The angle of twist is φ = TL/(GJ) in radians. Power and torque are linked by P = T·ω.

Polar moment and angle

J = π·15⁴/32 = 4970 mm⁴
φ = 1.48·π/180 = 0.02583 rad

Shear modulus

T = 20 N·m = 20000 N·mm
G = TL/(Jφ) = 20000·250/(4970·0.02583) = 38946 MPa
G = 38.95 GPa

Answer

G = 38.95 GPa

Compare: steel ≈ 80 GPa, brass ≈ 39 GPa, aluminium ≈ 26 GPa.

4.Torsion of shafts

Answer: d = 28.97 mm

Torsion of circular shafts: shear stress grows linearly from zero at the centre to τmax = T·r/J at the surface, with J = πd⁴/32 for a solid shaft and J = π(do⁴ − di⁴)/32 for a hollow one. The angle of twist is φ = TL/(GJ) in radians. Power and torque are linked by P = T·ω.

Torque

ω = 2πN/60 = 2π·750/60 = 78.54 rad/s
T = P/ω = 30000/78.54 = 382 N·m

Diameter from the allowable stress

d = ∛(16T/(π·τallow)) = ∛(16·381972/(π·80)) = 28.97 mm

Answer

d = 28.97 mm

In practice you would round up to the next standard size.

5.Mohr’s circle & stress transformation

Answer: σy′ = −12.32 MPa

Plane stress transformation: on a plane rotated by θ, σ = (σₓ + σᵧ)/2 + (σₓ − σᵧ)/2·cos 2θ + τₓᵧ·sin 2θ. Mohr’s circle shows all planes at once: its centre is at C = (σₓ + σᵧ)/2 and its radius is R = √(((σₓ − σᵧ)/2)² + τₓᵧ²). The principal stresses are C ± R, and the largest in-plane shear stress is R.

Transformation equation for the y′ face

σy′ = 0 − (−10)·0.5 − (−20)·(−0.866) = −12.32 MPa

Check

The sum of the normal stresses does not change with rotation.

σx′ = 12.32 MPa, σx′ + σy′ = 0 = σx + σy

Answer

σy′ = −12.32 MPa
6.Mohr’s circle & stress transformation

Answer: τθ = 43.5 MPa

Plane stress transformation: on a plane rotated by θ, σ = (σₓ + σᵧ)/2 + (σₓ − σᵧ)/2·cos 2θ + τₓᵧ·sin 2θ. Mohr’s circle shows all planes at once: its centre is at C = (σₓ + σᵧ)/2 and its radius is R = √(((σₓ − σᵧ)/2)² + τₓᵧ²). The principal stresses are C ± R, and the largest in-plane shear stress is R.

Transformation equation

τθ = −−20·0.6428 + 40·0.766 = 43.5 MPa

Answer

τθ = 43.5 MPa
7.Axial stress & strain

Answer: P = 41.89 kN

Two materials: in series (one after the other) every segment carries the same force and the elongations add: δ = P·Σ L/(E·A). In parallel (side by side between rigid plates) both parts shorten by the same amount, so their strains are equal: the stiffer part takes the larger share, Pi = P·EiAi/ΣEA, and σi = Ei·ε. A bar held between two rigid walls with a load at the junction is statically indeterminate: the two segments share the load in proportion to their stiffness k = EA/L.

Areas

A₁ = 314.2 mm², A₂ = 1257 mm²

Flexibilities

L₁/(E₁A₁) = 500/(200000·314.2) = 7.958 × 10⁻⁶ mm/N
L₂/(E₂A₂) = 200/(100000·1257) = 1.592 × 10⁻⁶ mm/N

Load

P = 0.4/9.549 × 10⁻⁶ = 41888 N = 41.89 kN

Answer

P = 41.89 kN
8.Axial stress & strain

Answer: σ2 = 7.596 MPa

Two materials: in series (one after the other) every segment carries the same force and the elongations add: δ = P·Σ L/(E·A). In parallel (side by side between rigid plates) both parts shorten by the same amount, so their strains are equal: the stiffer part takes the larger share, Pi = P·EiAi/ΣEA, and σi = Ei·ε. A bar held between two rigid walls with a load at the junction is statically indeterminate: the two segments share the load in proportion to their stiffness k = EA/L.

Stiffnesses

k₁ = 200000·490.9/500 = 196350 N/mm
k₂ = 70000·2827/400 = 494801 N/mm

Share of segment 2

F2 = 30000·494801/691150 = 21477 N

Stress

σ2 = 21477/2827 = 7.596 MPa (compression)

Answer

σ2 = 7.596 MPa
9.Column buckling

Answer: Pcr = 3.052 kN

Euler buckling: a slender column becomes unstable at Pcr = π²EI/(KL)², where KL is the effective length: K = 1 for pinned–pinned, 2 for fixed–free, 0.7 for fixed–pinned and 0.5 for fixed–fixed. It buckles about the axis with the smallest I. The formula holds for slender columns, whose critical stress stays below the yield stress.

Smallest second moment of area

A round section has the same I about every axis.

I = πd⁴/64 = π·30⁴/64 = 39761 mm⁴

Effective length

KL = 1·3000 = 3000 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·39761/3000² = 3052 N = 3.052 kN

Answer

Pcr = 3.052 kN
10.Column buckling

Answer: d = 79.34 mm

Euler buckling: a slender column becomes unstable at Pcr = π²EI/(KL)², where KL is the effective length: K = 1 for pinned–pinned, 2 for fixed–free, 0.7 for fixed–pinned and 0.5 for fixed–fixed. It buckles about the axis with the smallest I. The formula holds for slender columns, whose critical stress stays below the yield stress.

Required critical load

Pcr = n·P = 2·30000 = 60000 N
KL = 2·4000 = 8000 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·60000·8000²/(π³·200000))^(1/4) = 79.34 mm

Answer

d = 79.34 mm

Check: the slenderness KL/r is 403.3, so the column is slender and Euler applies.

11.Mechanical vibrations

Answer: ζ = 0.09999

Free vibration of a mass–spring system: the undamped natural frequency is ωn = √(k/m) in rad/s, and fn = ωn/(2π) in Hz. A viscous damper c gives the damping ratio ζ = c/cc, with critical damping cc = 2·√(k·m) = 2·m·ωn. An underdamped system (ζ < 1) oscillates at ωd = ωn·√(1 − ζ²). Springs in parallel add, k = k₁ + k₂; springs in series add as reciprocals, 1/k = 1/k₁ + 1/k₂.

Logarithmic decrement

δ = (1/4)·ln(40/3.2) = 0.6314

Damping ratio

ζ = δ/√(4π² + δ²) = 0.6314/√(39.48 + 0.3987) = 0.09999

Answer

ζ = 0.09999
12.Mechanical vibrations

Answer: fn = 2.531 Hz

Free vibration of a mass–spring system: the undamped natural frequency is ωn = √(k/m) in rad/s, and fn = ωn/(2π) in Hz. A viscous damper c gives the damping ratio ζ = c/cc, with critical damping cc = 2·√(k·m) = 2·m·ωn. An underdamped system (ζ < 1) oscillates at ωd = ωn·√(1 − ζ²). Springs in parallel add, k = k₁ + k₂; springs in series add as reciprocals, 1/k = 1/k₁ + 1/k₂.

Equivalent stiffness

Only k1 and k2 are in parallel. That pair is in series with k3, so combine them as reciprocals.

k12 = 12 + 5 = 17 kN/m
keq = 17·25/(17 + 25) = 10.12 kN/m

Natural frequency

ωn = √(10119/40) = 15.91 rad/s
fn = 15.91/(2π) = 2.531 Hz

Answer

fn = 2.531 Hz

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